US20250003483A1 - Planetary gearbox with a thrust washer having anti-rotation means - Google Patents
Planetary gearbox with a thrust washer having anti-rotation means Download PDFInfo
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- US20250003483A1 US20250003483A1 US18/710,328 US202218710328A US2025003483A1 US 20250003483 A1 US20250003483 A1 US 20250003483A1 US 202218710328 A US202218710328 A US 202218710328A US 2025003483 A1 US2025003483 A1 US 2025003483A1
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- Prior art keywords
- planet
- thrust washer
- thrust
- washer
- housing
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/04—Features relating to lubrication or cooling or heating
- F16H57/048—Type of gearings to be lubricated, cooled or heated
- F16H57/0482—Gearings with gears having orbital motion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
- F16C33/1025—Construction relative to lubrication with liquid, e.g. oil, as lubricant
- F16C33/106—Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
- F16C33/1065—Grooves on a bearing surface for distributing or collecting the liquid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/04—Features relating to lubrication or cooling or heating
- F16H57/0467—Elements of gearings to be lubricated, cooled or heated
- F16H57/0479—Gears or bearings on planet carriers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/08—General details of gearing of gearings with members having orbital motion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/08—General details of gearing of gearings with members having orbital motion
- F16H57/082—Planet carriers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2361/00—Apparatus or articles in engineering in general
- F16C2361/61—Toothed gear systems, e.g. support of pinion shafts
Definitions
- the present disclosure relates to a planetary gearbox having a housing, with planet gears and with planet bearings.
- the planet gears are mounted on the housing by means of the planet bearings so as to be rotatable about an axially aligned planetary axis and at least one of the planet bearings is formed from at least one axially aligned planet pin and a thrust washer.
- the thrust washer is seated axially between the planet gear and the housing on the planet pin and is held in a form-fitting manner with the aid of an anti-rotation means so as to prevent rotation about the planetary axis and relative to the housing.
- the thrust washers are axial sliding bearings of the planet bearings for the respective planet gear.
- the planet gear is mounted radially on a planet bolt by means of the planet bearing.
- the thrust washers are seated axially between the planet bearing, the planet gear and the planet carrier.
- a bearing surface is defined via the surface of the respective thrust washer, which is usually designed as a sliding bearing surface.
- the sliding bearing surfaces are designed differently from case to case.
- the thrust washers are equipped with tongue-like anti-rotation means. This prevents the respective thrust washer from rotating in relation to the planet carrier and avoids frictional wear in the contact zone between the hard thrust washer and the usually non-hardened planet carrier. On the other hand, undefined friction or sliding conditions between the thrust washer and the planet gear are avoided.
- the present disclosure provides a planetary gearbox which can be produced easily and inexpensively.
- the thrust washer has first thrust surfaces on a first side facing the housing and second thrust surfaces offset circumferentially relative to the first thrust surfaces on a second side facing a planet gear. Furthermore, a trough-like lubrication channel is formed on the thrust washer axially on the rear side of the thrust surfaces in each case. The lubrication channel extends radially outwards from the direction of the planet pin as far as an edge which delimits the thrust washer radially on the outside.
- the lubrication channel extends in each case between two of the first thrust surfaces of the thrust washer which are circumferentially adjacent to one another.
- the lubrication channel ends at at least one of the anti-rotation means of a thrust washer.
- a design of the planetary gearbox is assumed in which at least one housing section of the housing is formed as a planet carrier and the housing sections are support cheeks of the planet carrier connected axially by means of connecting pieces.
- the stop is a connecting piece projecting axially from one support cheek of the planet carrier in the direction of a further support cheek.
- each of the connecting pieces has at least one stop for one anti-rotation means formed on one and the same thrust washer of two anti-rotation means formed on the thrust washer.
- two flanks of the planet carrier facing away from one another are the stops for the anti-rotation means of a thrust washer.
- the stops are formed circumferentially between two adjacent connecting pieces and adjoining the planet pin.
- the thrust washer has two anti-rotation means which extend radially from a washer body and are formed circumferentially about a planetary axis of a planet gear adjacent to one another on the washer body and are made of a material of the thrust washer.
- the anti-rotation means may be integrally formed with a washer body of the thrust washer.
- the material may be sheet steel.
- a first anti-rotation means rests against a first stop.
- a second anti-rotation means formed on the same thrust washer rests against a second stop opposite the first stop.
- the respective stop may be formed on a connecting piece of a planet carrier of the planetary gearbox. Two support cheeks of the planet carrier are connected to one another via the respective connecting piece.
- At least one of the anti-rotation means projects radially away from the planet pin beyond a contour of the planet gear, which contour delimits the planet gear on the outside.
- At least one of the anti-rotation means projects radially away from the planet pin beyond a contour of the planet gear, which contour delimits the at least one planet gear on the outside.
- the lubrication channel which is delimited on at least one side by the thrust washer, extends radially outwards as far as an edge of the anti-rotation means, which delimits the thrust washer radially on the outside.
- the disclosure also provides for a thrust washer for the planetary gearbox.
- the thrust washer has first bulges and second bulges circumferentially adjacent to the first bulges.
- the first thrust surfaces are separated from one another by first bulges of the thrust washer.
- the second thrust surfaces are formed on the first bulges on the second side and rear side and are separated from one another by second bulges of the thrust washer.
- the first thrust surfaces are formed on the second bulges on the first side and rear side.
- a first bulge and a second bulge are, in each case, connected to one another by an elbowed section, which ensures the axial offset of the thrust surfaces.
- the bulges extend radially outwards in a trough-like manner from the direction of the planet pins as far as an edge of the thrust washer which delimits the thrust washer radially on the outside.
- the bulges may continue radially beyond an outer circumference of the washer body of the thrust washer and further at least partially into the anti-rotation means or, for example, up to the outer contour of the thrust washer on the anti-rotation means.
- Two anti-rotation means are formed on the thrust washer instead of just one. This results in more possibilities for securing the thrust washer so as to prevent rotation. A targeted mounting of the thrust washer can be dispensed with in most cases.
- the thrust washer is supported against rotation by means of the respective anti-rotation means, either on one or two stops. Due to the aforementioned design of the axial washer, it is identical on both axially directed end faces and also mirror-symmetrical with respect to the anti-rotation means so that it can be mounted in the planet carrier without the need for a directionally oriented mounting.
- the stop is a connecting piece that connects the housing sections, e.g., the support cheeks of a planet carrier, with one another, which alternatively also forms more than one stop.
- these connecting pieces are already present in any case, the complex production of additional form-fit recesses for the engagement of the anti-rotation means of the thrust washers can advantageously be dispensed with.
- Housings are housings of vehicle transmissions, of electric motors or of drive units operated by electric motors—but are alternatively also planet carriers and differential cases, e.g., differential cases of spur gear differentials. Accordingly, housing sections are, for example, end shields, partition walls, solid housings, halves of differential cases or support cheeks of planet carriers.
- the stop protrudes at least partially axially into a gap between planet gears distributed circumferentially around the central axis and adjacent to one another. This means that no additional effort is required for the positional orientation of the anti-rotation means.
- the connecting pieces which are already circumferentially adjacent to one another, can be used as stops.
- the thrust washer according to the disclosure is designed such that the stop radially adjoins the planet pin and projects radially beyond a contour of the housing.
- the position of the stop is therefore not essentially linked to the circumference of the planet gear, as is the case with known planet bearings, but is independent of it.
- the anti-rotation means and the stop can have two stop sides pointing away from one another and in opposite circumferential directions, each serving to abut, in each case, a different anti-rotation means of one and the same thrust washer.
- the bulges on the thrust washers interact with a further component to create lubrication channels, which can optionally form channels delimited by further thrust washers, housing sections, sections of the planet carrier or flanks of planet gears. Through these channels, lubricating oil reaching the thrust washer can be conveyed from the thrust washers on the inside radially to the outside without any additional effort.
- the thrust washers are provided with anti-rotation means for the reasons already mentioned in the “BACKGROUND” section.
- the anti-rotation means engages in a form-fitting manner in a form-fit recess prepared on the respective housing, for example in a hole, an indentation or a recess.
- the thrust washers must be aligned, held and positioned with respect to the form-fit recesses when mounting the planet bearings with the anti-rotation means. This is often associated with increased effort-on the one hand, because the respective form-fit recess must be introduced into the housing and, on the other hand, because the directional positioning requires specific devices and operations for assembly.
- the aim is to handle planet gears together with the planet bearing (needle or roller bearing), with the planet pin/planet bolt and with the thrust washer as an assembly. This is possible by implementing the disclosed device with the planetary gearboxes according to the disclosure.
- axial is understood as aligned with the central axis 9 of the planetary gearbox 1 or 21 .
- radial is understood as transverse to the axial direction.
- FIG. 1 shows a general view of an exemplary embodiment of a planetary gearbox 1 with a lateral view of one side of the planetary gearbox 1 .
- FIG. 2 shows a detail from FIG. 1 with a planet bearing 4 , enlarged and not shown to scale.
- FIG. 3 shows a detail of the arrangement shown in FIG. 1 in an exposed view, in which the base body 33 of a support cheek 12 in the foreground in FIG. 1 is omitted.
- FIG. 4 shows a general view of an exemplary embodiment of a planetary gearbox 21 with a lateral view of one side of the planetary gearbox 21 .
- FIG. 5 shows a detail from FIG. 4 with a position of a planet gear 3 , enlarged and not shown to scale.
- FIG. 6 schematically shows an assembly of the planetary gearbox 1 .
- FIG. 7 shows a frontal view of a further exemplary embodiment of a planetary gearbox 50 with a view of the support cheek 12 from the front.
- FIG. 8 shows a frontal view of an exemplary embodiment of a thrust washer 48 installed in the planetary gearbox 50 as an individual component.
- FIG. 9 shows a longitudinal section through the thrust washer 48 along the line IX-IX drawn in FIG. 8 .
- FIG. 10 shows a longitudinal section through the thrust washer 48 along the line X-X drawn in FIG. 1 .
- FIG. 1 shows a planetary gearbox 1 with a housing 2 , planet gears 3 and planet bearings 4 .
- the housing 2 is a planet carrier 7 , which is formed from a case-like support cheek 12 and a support cheek 14 with a flange 25 .
- a plate-like base body 33 of the support cheek 12 is provided with axially aligned connecting pieces 13 .
- the support cheek 12 is connected to the support cheek 14 via the connecting pieces 13 .
- the flange 25 has through-holes 26 for fastening the planetary gearbox 1 .
- Pocket-like windows 27 are formed between the connecting pieces 13 .
- the toothing 29 of a planet gear 3 protrudes from each of the windows 27 .
- the planet gears 3 are arranged in the support cheek 12 axially between the support cheek 12 and the support cheek 14 and at equal distances from one another around the central axis 9 , each distributed with a radial distance between its planetary axis 24 and the central axis 9 .
- the planet gears 3 are mounted with planet pins 5 on one side in the support cheek 12 and on the other side in the support cheek 14 .
- one thrust washer 6 is arranged between the respective planet gear 3 and the support cheek 12 or 14 , which is largely concealed in the illustration, the anti-rotation means 8 of which project radially beyond the contour 18 of the toothing 29 and are opposite a stop 10 .
- Each of the connecting pieces 13 is a stop 10 or forms a stop 10 for, in each case, four of the anti-rotation means 8 and thus for four thrust washers 6 .
- two of the thrust washers 6 are, in each case, assigned to one window 27 and two of the thrust washers 6 are assigned to an adjacent window 27 .
- FIGS. 1 and 2 Of the planet bearings 4 , in each case only the end faces of the planet pins 5 and anti-rotation means 8 of the thrust washers 6 , which are almost concealed in the view, are visible.
- the planet pins 5 are designed as planet bolts on which the planet gears 3 are mounted such that they can rotate about the planetary axes 24 .
- the planet pins 5 can also be formed integrally/in one piece with the planet gears 3 .
- the thrust washers 6 are provided with tongue-like projections which project radially beyond the toothing 29 of the respective planet gear 3 and which form an anti-rotation means 8 at the stops 10 .
- the connecting pieces 13 are the stops 10 .
- FIG. 6 The thrust washers 6 are made of sheet metal.
- a thrust washer 6 is shown as an individual component positioned on a planet gear 3 .
- the other thrust washer 6 is concealed by the gear 3 .
- the thrust washer 6 has a washer body 28 which surrounds a through-hole 32 .
- Axial recesses 31 are formed on the washer body 28 .
- Two tongue-like anti-rotation means 8 project radially from the washer body 28 .
- the first side 40 of the thrust washer 6 facing away from the planet gear 3 and facing towards the housing 3 or the planet carrier 7 during installation has first thrust surfaces 39 .
- the thrust surfaces 39 are formed on the front side of the axial bulges 42 .
- These bulges 42 form trough-like lubrication channels 43 on the rear side of the thrust surfaces 39 and limit an oil passage with the planet gear 3 , which extends through the lubrication channel 43 on the inside from the through-hole 32 radially 30 ) outwards to the edge 44 .
- the second side 46 of the thrust washer 6 which faces the planet gear 3 and is concealed in the illustration, is provided with second thrust surfaces 38 , which are concealed in the illustration and which are formed on the front side of the bulges 41 .
- the front side lies in the direction in which the bulge 41 is axially curved and closes it off axially.
- the bulges 41 form lubrication channels 43 open to the top and, in the installed state (see FIG. 1 ), together with the planet carrier 7 , limit the oil passage, which extends radially outwards on the inside from the through-hole 32 to the edge 44 of the thrust washer 6 .
- some of the lubrication channels 43 end radially on the anti-rotation means 8 as seen in the radial direction, which in both cases continues in the radial direction from the radial end of the bulge 41 or 42 in the radial direction projecting beyond the washer body 28 .
- FIG. 3 A view is shown from the axial direction of the thrust washer 6 of a planet bearing 4 in an imaginary and not shown radial plane, wherein the radial plane extends axially between the base body 33 of the support cheek 12 cut out of this view and the thrust washer 6 .
- the thrust washer 6 is guided on the planet pin 5 via edge sections 34 of the through-hole 32 or the washer body 28 .
- the edge sections 34 delimit the indentations 30 on the edge in the circumferential direction around the planetary axis 24 .
- the indentations 30 connect radially on the inside to lubrication grooves 35 in the thrust washer 6 .
- the respective planet pin 5 is a planet bolt and is mounted in the support cheek 14 visible in the background of the illustration and in the foreground (not shown) in the support plate 12 .
- the respective planetary axis 24 extends axially and, in the representation according to FIG. 3 , vertically into the image plane.
- a planet gear 3 follows the respective thrust washer 6 in the viewing direction.
- Anti-rotation means 8 of a thrust washer 6 which is concealed by the planet gear 3 and arranged axially between the planet gear 3 and the support cheek 14 , are visible in the background of the illustration.
- the two thrust washers 6 are provided with the anti-rotation means 8 , which protrude radially as tongues from the sheet metal of the thrust washer 6 .
- the tongues form an angle of 120° between them in a circumferential direction, which can alternatively also be greater or less than 120°.
- a gap 11 is formed between two opposing planet gears 3 .
- One of the connecting pieces 13 which forms one or more of the stops 10 , extends between the support cheeks 12 and 14 in every gap 11 .
- the stop 10 is formed on a flank of the connecting piece 13 facing the planet gear 3 . It is also conceivable that two of the connecting pieces extend in a gap.
- a pivoting clearance is formed between the anti-rotation means 8 and 30 ) the connecting pieces 13 , by which the thrust washer 6 can pivot on the planet bolt about the planetary axis 24 up to the respective stop 10 so that one of the anti-rotation means 8 of the respective thrust washer can abut against the stop 10 opposite to it or none of the anti-rotation means 10 can come into contact. Lubrication channels 43 formed in the thrust washer 6 are visible here.
- FIG. 4 A planetary gearbox 21 with a housing 2 , planet gears 3 and planet bearings 4 a is shown.
- the housing 2 is a planet carrier 7 , which is formed from a case-like support cheek 12 and a support cheek 14 with a flange 25 .
- a plate-like base body 33 of the support cheek 12 is provided with axially aligned connecting pieces 13 .
- the support cheek 12 is connected to the support cheek 14 via the connecting pieces 13 .
- the flange 25 has through-holes 26 for fastening the planetary gearbox 21 .
- Pocket-like windows 27 are formed between the connecting pieces 13 .
- the toothing 29 of a planet gear 3 protrudes from each of the windows 27 .
- the planet gears 3 are arranged axially between the support cheek 12 and the support cheek 14 and are distributed at equal distances from one another in the case of the support cheek 12 .
- the planet gears 3 are mounted with planet pins 5 on one side in the support cheek 12 and on the other side in the support cheek 14 .
- the planet gears 3 are rotatably mounted on the housing 2 by means of the planet bearings 4 a .
- the respective planet bearing 4 a is formed from the axially aligned planet pin/planet bolt 5 and a thrust washer 6 a .
- the thrust washer 6 a sits axially between the planet gear 3 and the housing 2 on the planet pin 5 , is provided with two anti-rotation means 8 a , and is held by these anti-rotation means 8 a against rotation relative to the housing 2 in a form-fitting manner against a stop 10 a.
- the stop 10 a is formed circumferentially between two adjacent connecting pieces 13 and projects radially beyond a contour of the base body 33 of the support cheek 12 , adjoining the planet pin 5 radially on the outside, when viewed in the radial direction from the center of the planetary gearbox 21 . More precisely, the stops 10 a for, in each case, one of the thrust washers 6 a are circumferentially formed on the flanks of the planet carrier 7 facing away from one another between two adjacent connecting pieces 13 and adjoining the respective planet pin 5 .
- the flanks are body edges or surfaces, directed in the circumferential direction, of a radially projecting support section of the support cheek 12 , at which the planet pins 5 are partly accommodated in the support cheek 12 .
- FIG. 5 The illustration shows sections of the housing 2 formed as a planet carrier 7 , the support cheek 14 and the support cheek 12 .
- the respective stop 10 a projecting radially from the base body 33 has stop surfaces 19 and 20 .
- a partial surface of the respective stop surface 19 or 20 is opposite the flank of a connecting piece 13 .
- a further tongue of a further anti-rotation means 8 a also curved in the manner of a wing at the end engages behind a second stop side 20 of the stop 10 a in the opposite circumferential direction, which stop side faces away from the first stop side 19 in the circumferential direction.
- the wings 22 of the anti-rotation means 8 a are angled slightly in an axial direction for this purpose.
- FIG. 7 The design of the planetary gearbox 50 is comparable to that of the planetary gearbox 1 shown in FIG. 1 , with the exception of differently designed thrust washers 48 , i.e., the thrust washers 6 of the planetary gearbox 1 shown in FIG. 1 can be exchanged for the thrust washers 48 and vice versa without further structural changes.
- the thrust washers 48 are provided with lubrication channels 51 formed by lubrication grooves 52 , each of which ends at an anti-rotation means 49 and, where the anti-rotation means 49 are no longer axially opposite the housing 2 , continues in a lubrication groove 52 to the end of the anti-rotation means 49 .
- the thrust washer has first bulges 53 and second bulges 54 circumferentially adjacent to the first bulges 53 .
- the bulges are axial recesses created by embossing from a disc-like washer body 55 lying flat in a radial plane.
- the first bulges 53 are curved vertically into the image plane in the representation according to FIG. 8 and are curved out axially to the left from the radial plane E 1 according to the representation of FIG. 9 .
- the second bulges 54 rise vertically into the image plane towards the viewer and are correspondingly curved out axially to the right from the radial plane E 2 according to the representation of FIG.
- First thrust surfaces 38 are formed on the front side of the first bulges 53 , each of which is concealed behind the rear side 53 a of the bulge 53 in the representation according to FIG. 8 .
- the thrust surfaces 39 are formed on the front side of the second bulges 54 .
- the thrust surfaces 39 are, in each case, separated from one another by a bulge 53 and the thrust surfaces 38 are separated by a bulge 54 .
- a first bulge 53 and a second bulge 54 are, in each case, connected to one another by an elbowed section 45 .
- FIG. 8 The thrust washer 48 has two anti-rotation means 49 extending radially from a washer body 55 and formed circumferentially around the center axis or axis of symmetry 24 of a planet gear adjacent to one another on the washer body 55 , which are formed integrally/in one piece with the washer body 55 .
- the contour of the anti-rotation means 49 projects radially beyond an outer circumferential line U of the washer body 55 of the thrust washer 48 .
- the washer body 55 is annularly delimited on the inside by the contours of the through-hole with the indentations 30 and on the outside by the outer circumferential line U and has an outer diameter DU of the outer circumferential line U.
- the washer body 55 is designed to be symmetrical with respect to the axes of symmetry S 1 and S 2 .
- the axis of symmetry S 1 is aligned horizontally and the axis of symmetry S 2 is aligned vertically.
- the axes of symmetry S 1 and S 2 lie in a radial plane which is pierced perpendicularly by the planetary axis 24 .
- the axes of symmetry S 1 and S 2 extend perpendicular to one another and intersect at a common point on the planetary axis 24 .
- the contour of the anti-rotation means 49 is defined, in each case, by two flank lines F 1 and F 2 .
- Each contour of one of the anti-rotation means 49 is therefore outlined in the image plane by a flank line F 1 and a flank line F 2 as well as an arc.
- the arc connects the flank lines F 1 and F 2 of an anti-rotation means 49 .
- the anti-rotation means 49 are designed to be symmetrical to one another and are mirrored on the axis of symmetry S 2 .
- flank lines F 1 of the two anti-rotation means 49 intersect at a common intersection point C 1 , which lies on the extension of the axis of symmetry S 2 and which lies, at a radial distance from the outer contour of the thrust washer 48 , outside of the outer contour.
- the flank lines F 1 and F 1 of the adjacent anti-rotation means 49 form an obtuse angle W 1 between them and the flank lines F 1 and F 2 form an acute angle W 2 between them and the axis of symmetry S 2 on one of the anti-rotation means 49 in each case.
- the two flank lines F 1 of both anti-rotation means 49 optionally merge at a straight line describing the outer contour of the thrust washer at this point and extending radially below the intersection point C 1 or alternatively at an arcuate line (not shown) of the outer contour of the thrust washer 48 .
- the respective extension of the flank line F 1 of the one anti-rotation means 49 intersects the extension of its flank line F 2 at an intersection point C 2 , which lies on the axis of symmetry S 1 and radially outside of the outer contour of the thrust washer 48 .
- the contour lines F 1 and F 2 of the respective anti-rotation means 49 form an acute angle W 2 between them.
- the thrust washer 48 is geometrically divided into quarter sections 48 a - 48 d .
- the quarter sections 48 a - 48 d adjoin one another at the axes of symmetry S 1 and S 2 and are designed to be symmetrical to one another on the washer body 55 described by the circumferential line U.
- the outer contours of the quarter 30 ) sections 48 a and 48 b lying above the axis of symmetry S 1 are each delimited radially outwards by a complete flank line F 1 and a part of a flank line F 2 .
- the outer contours of the quarter sections 48 c and 48 d are each delimited by a part of a flank line F 2 and a part of an arc line.
- the arc line lies on the circumferential line U.
- the respective flank line F 2 merges into the arc line in the respective quarter section 48 c and 48 d , so that the contours of the anti-rotation means also extend, in each case, into the quarter section 48 c or 48 d lying below the axis of symmetry S 1 .
- the radius of the arc line starting from the planetary axis 24 corresponds to half the diameter DU of the outer circumferential line.
- each of the quarter sections 48 a - 48 d one of the bulges 54 is fully formed once.
- Each of the quarter sections 48 a - 48 d also has, twice in each case, a part of one of the bulges 53 .
- the bulges 54 of the quarter sections 48 a and 48 b continue in the anti-rotation means 49 up to the outer contour of the thrust washer 48 and thus the anti-rotation means 49 at that point.
- a bulge 53 which extends along the axis of symmetry S 1 and is formed partially in a quarter section 48 a and 48 d or 48 b and 48 d , continues radially outwards as far as the outer contour of the respective anti-rotation means 49 and thus the outer contour of the thrust washer 48 .
- At least one lubrication channel ( 43 ) delimited on at least one side by the thrust washer ( 48 ) extends radially outwards to partial sections of the contour lines F 1 , F 2 of the outer contours of the anti-rotation means 49 delimiting the anti-rotation means 49 radially on the outside—i.e., that the lubrication channel 43 or the bulges 53 , 54 continue radially to the end/to the tip of the anti-rotation means 49 via the contact with the planet gear and/or the planet carrier.
- FIGS. 9 and 10 The sheet metal of the thrust washer 48 has a sheet thickness D.
- the total thickness A of the thrust washer 48 is composed of the sheet thickness D and the axial offset T.
- the axial offset T is a measure of the depth of the bulges 53 and 54 and is less than the sheet thickness D in this case.
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- General Engineering & Computer Science (AREA)
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- Oil, Petroleum & Natural Gas (AREA)
- General Details Of Gearings (AREA)
- Retarders (AREA)
Abstract
A planetary gearbox includes a housing having a pair of stops, a planet bearing mounted in the housing, and a planet gear rotatable on the planet bearing. The planet bearing is formed from an axially aligned planet pin and a thrust washer. The thrust washer includes two integrally-formed projections, each facing one of the stops to prevent rotation of the thrust washer about the planetary axis. The thrust washer also includes first thrust surfaces disposed on a first side of the thrust washer facing the housing, first lubrication channels formed axially opposite the first thrust surfaces and extending radially outwards, second thrust surfaces circumferentially offset from the first thrust surfaces and disposed on a second side of the thrust washer facing the planet gear, and second lubrication channels formed axially opposite the second thrust surfaces and extending radially outwards.
Description
- This application is the United States National Phase of PCT Appln. No. PCT/DE2022/100868 filed Nov. 21, 2022, which claims priority to German Application No. DE102021131137.3 filed Nov. 26, 2021, the entire disclosures of which are incorporated by reference herein.
- The present disclosure relates to a planetary gearbox having a housing, with planet gears and with planet bearings. The planet gears are mounted on the housing by means of the planet bearings so as to be rotatable about an axially aligned planetary axis and at least one of the planet bearings is formed from at least one axially aligned planet pin and a thrust washer. The thrust washer is seated axially between the planet gear and the housing on the planet pin and is held in a form-fitting manner with the aid of an anti-rotation means so as to prevent rotation about the planetary axis and relative to the housing.
- Such a planetary gearbox is disclosed in DE 40 09 968 A1. The thrust washers are axial sliding bearings of the planet bearings for the respective planet gear. The planet gear is mounted radially on a planet bolt by means of the planet bearing. The thrust washers are seated axially between the planet bearing, the planet gear and the planet carrier. A bearing surface is defined via the surface of the respective thrust washer, which is usually designed as a sliding bearing surface. The sliding bearing surfaces are designed differently from case to case. The thrust washers are equipped with tongue-like anti-rotation means. This prevents the respective thrust washer from rotating in relation to the planet carrier and avoids frictional wear in the contact zone between the hard thrust washer and the usually non-hardened planet carrier. On the other hand, undefined friction or sliding conditions between the thrust washer and the planet gear are avoided.
- The present disclosure provides a planetary gearbox which can be produced easily and inexpensively.
- According to the disclosure, the thrust washer has first thrust surfaces on a first side facing the housing and second thrust surfaces offset circumferentially relative to the first thrust surfaces on a second side facing a planet gear. Furthermore, a trough-like lubrication channel is formed on the thrust washer axially on the rear side of the thrust surfaces in each case. The lubrication channel extends radially outwards from the direction of the planet pin as far as an edge which delimits the thrust washer radially on the outside.
- In one embodiment, the lubrication channel extends in each case between two of the first thrust surfaces of the thrust washer which are circumferentially adjacent to one another.
- In a further embodiment, the lubrication channel ends at at least one of the anti-rotation means of a thrust washer.
- In one embodiment, a design of the planetary gearbox is assumed in which at least one housing section of the housing is formed as a planet carrier and the housing sections are support cheeks of the planet carrier connected axially by means of connecting pieces. In such a planetary gearbox, the stop is a connecting piece projecting axially from one support cheek of the planet carrier in the direction of a further support cheek.
- In a further development of the aforementioned embodiment, each of the connecting pieces has at least one stop for one anti-rotation means formed on one and the same thrust washer of two anti-rotation means formed on the thrust washer.
- In addition, in a further development, two flanks of the planet carrier facing away from one another are the stops for the anti-rotation means of a thrust washer. The stops are formed circumferentially between two adjacent connecting pieces and adjoining the planet pin.
- In a further embodiment, the thrust washer has two anti-rotation means which extend radially from a washer body and are formed circumferentially about a planetary axis of a planet gear adjacent to one another on the washer body and are made of a material of the thrust washer. The anti-rotation means may be integrally formed with a washer body of the thrust washer. The material may be sheet steel. A first anti-rotation means rests against a first stop. A second anti-rotation means formed on the same thrust washer rests against a second stop opposite the first stop. The respective stop may be formed on a connecting piece of a planet carrier of the planetary gearbox. Two support cheeks of the planet carrier are connected to one another via the respective connecting piece.
- In a further embodiment, at least one of the anti-rotation means projects radially away from the planet pin beyond a contour of the planet gear, which contour delimits the planet gear on the outside.
- In one embodiment, at least one of the anti-rotation means projects radially away from the planet pin beyond a contour of the planet gear, which contour delimits the at least one planet gear on the outside. In this regard, the lubrication channel, which is delimited on at least one side by the thrust washer, extends radially outwards as far as an edge of the anti-rotation means, which delimits the thrust washer radially on the outside.
- The disclosure also provides for a thrust washer for the planetary gearbox. The thrust washer has first bulges and second bulges circumferentially adjacent to the first bulges. The first thrust surfaces are separated from one another by first bulges of the thrust washer. The second thrust surfaces are formed on the first bulges on the second side and rear side and are separated from one another by second bulges of the thrust washer. The first thrust surfaces are formed on the second bulges on the first side and rear side. A first bulge and a second bulge are, in each case, connected to one another by an elbowed section, which ensures the axial offset of the thrust surfaces. The bulges extend radially outwards in a trough-like manner from the direction of the planet pins as far as an edge of the thrust washer which delimits the thrust washer radially on the outside. The bulges may continue radially beyond an outer circumference of the washer body of the thrust washer and further at least partially into the anti-rotation means or, for example, up to the outer contour of the thrust washer on the anti-rotation means.
- Two anti-rotation means are formed on the thrust washer instead of just one. This results in more possibilities for securing the thrust washer so as to prevent rotation. A targeted mounting of the thrust washer can be dispensed with in most cases. The thrust washer is supported against rotation by means of the respective anti-rotation means, either on one or two stops. Due to the aforementioned design of the axial washer, it is identical on both axially directed end faces and also mirror-symmetrical with respect to the anti-rotation means so that it can be mounted in the planet carrier without the need for a directionally oriented mounting.
- It is also provided that the stop is a connecting piece that connects the housing sections, e.g., the support cheeks of a planet carrier, with one another, which alternatively also forms more than one stop. As these connecting pieces are already present in any case, the complex production of additional form-fit recesses for the engagement of the anti-rotation means of the thrust washers can advantageously be dispensed with.
- Housings are housings of vehicle transmissions, of electric motors or of drive units operated by electric motors—but are alternatively also planet carriers and differential cases, e.g., differential cases of spur gear differentials. Accordingly, housing sections are, for example, end shields, partition walls, solid housings, halves of differential cases or support cheeks of planet carriers.
- In one embodiment, the stop protrudes at least partially axially into a gap between planet gears distributed circumferentially around the central axis and adjacent to one another. This means that no additional effort is required for the positional orientation of the anti-rotation means. The connecting pieces, which are already circumferentially adjacent to one another, can be used as stops.
- The thrust washer according to the disclosure is designed such that the stop radially adjoins the planet pin and projects radially beyond a contour of the housing. The position of the stop is therefore not essentially linked to the circumference of the planet gear, as is the case with known planet bearings, but is independent of it. Accordingly, there are a variety of design options for the anti-rotation means and the stop. For example, in one embodiment, the stop can have two stop sides pointing away from one another and in opposite circumferential directions, each serving to abut, in each case, a different anti-rotation means of one and the same thrust washer.
- The bulges on the thrust washers interact with a further component to create lubrication channels, which can optionally form channels delimited by further thrust washers, housing sections, sections of the planet carrier or flanks of planet gears. Through these channels, lubricating oil reaching the thrust washer can be conveyed from the thrust washers on the inside radially to the outside without any additional effort.
- In planetary gearboxes of the prior art, the thrust washers are provided with anti-rotation means for the reasons already mentioned in the “BACKGROUND” section. As such, the anti-rotation means engages in a form-fitting manner in a form-fit recess prepared on the respective housing, for example in a hole, an indentation or a recess. Accordingly, the thrust washers must be aligned, held and positioned with respect to the form-fit recesses when mounting the planet bearings with the anti-rotation means. This is often associated with increased effort-on the one hand, because the respective form-fit recess must be introduced into the housing and, on the other hand, because the directional positioning requires specific devices and operations for assembly.
- When assembling planetary gearboxes, the aim is to handle planet gears together with the planet bearing (needle or roller bearing), with the planet pin/planet bolt and with the thrust washer as an assembly. This is possible by implementing the disclosed device with the planetary gearboxes according to the disclosure.
- The present disclosure is described in more detail below with reference to the drawings.
- The term “axial” is understood as aligned with the
central axis 9 of the 1 or 21. The term “radial” is understood as transverse to the axial direction.planetary gearbox -
FIG. 1 shows a general view of an exemplary embodiment of aplanetary gearbox 1 with a lateral view of one side of theplanetary gearbox 1. -
FIG. 2 shows a detail fromFIG. 1 with aplanet bearing 4, enlarged and not shown to scale. -
FIG. 3 shows a detail of the arrangement shown inFIG. 1 in an exposed view, in which thebase body 33 of asupport cheek 12 in the foreground inFIG. 1 is omitted. -
FIG. 4 shows a general view of an exemplary embodiment of aplanetary gearbox 21 with a lateral view of one side of theplanetary gearbox 21. -
FIG. 5 shows a detail fromFIG. 4 with a position of aplanet gear 3, enlarged and not shown to scale. -
FIG. 6 schematically shows an assembly of theplanetary gearbox 1. -
FIG. 7 shows a frontal view of a further exemplary embodiment of aplanetary gearbox 50 with a view of thesupport cheek 12 from the front. -
FIG. 8 shows a frontal view of an exemplary embodiment of athrust washer 48 installed in theplanetary gearbox 50 as an individual component. -
FIG. 9 shows a longitudinal section through thethrust washer 48 along the line IX-IX drawn inFIG. 8 . -
FIG. 10 shows a longitudinal section through thethrust washer 48 along the line X-X drawn inFIG. 1 . -
FIG. 1 shows aplanetary gearbox 1 with ahousing 2, planet gears 3 andplanet bearings 4. Thehousing 2 is a planet carrier 7, which is formed from a case-like support cheek 12 and asupport cheek 14 with aflange 25. A plate-like base body 33 of thesupport cheek 12 is provided with axially aligned connectingpieces 13. Thesupport cheek 12 is connected to thesupport cheek 14 via the connectingpieces 13. Theflange 25 has through-holes 26 for fastening theplanetary gearbox 1. - Pocket-
like windows 27 are formed between the connectingpieces 13. Thetoothing 29 of aplanet gear 3 protrudes from each of thewindows 27. The planet gears 3 are arranged in thesupport cheek 12 axially between thesupport cheek 12 and thesupport cheek 14 and at equal distances from one another around thecentral axis 9, each distributed with a radial distance between itsplanetary axis 24 and thecentral axis 9. On the respective planet bearing 4, the planet gears 3 are mounted withplanet pins 5 on one side in thesupport cheek 12 and on the other side in thesupport cheek 14. In each case, onethrust washer 6 is arranged between therespective planet gear 3 and the 12 or 14, which is largely concealed in the illustration, the anti-rotation means 8 of which project radially beyond thesupport cheek contour 18 of thetoothing 29 and are opposite astop 10. Each of the connectingpieces 13 is astop 10 or forms astop 10 for, in each case, four of the anti-rotation means 8 and thus for fourthrust washers 6. Of the fourthrust washers 6, two of thethrust washers 6 are, in each case, assigned to onewindow 27 and two of thethrust washers 6 are assigned to anadjacent window 27. -
FIGS. 1 and 2 —Of theplanet bearings 4, in each case only the end faces of the planet pins 5 and anti-rotation means 8 of thethrust washers 6, which are almost concealed in the view, are visible. In the example shown, it is assumed that the planet pins 5 are designed as planet bolts on which the planet gears 3 are mounted such that they can rotate about theplanetary axes 24. Alternatively, the planet pins 5 can also be formed integrally/in one piece with the planet gears 3. Thethrust washers 6 are provided with tongue-like projections which project radially beyond thetoothing 29 of therespective planet gear 3 and which form an anti-rotation means 8 at thestops 10. As already mentioned above, the connectingpieces 13 are thestops 10. -
FIG. 6 —Thethrust washers 6 are made of sheet metal. In this illustration, athrust washer 6 is shown as an individual component positioned on aplanet gear 3. Theother thrust washer 6 is concealed by thegear 3. Of theconcealed thrust washer 6, only the anti-rotation means 8 are visible. Thethrust washer 6 has awasher body 28 which surrounds a through-hole 32. Axial recesses 31 are formed on thewasher body 28. Two tongue-like anti-rotation means 8 project radially from thewasher body 28. Thefirst side 40 of thethrust washer 6 facing away from theplanet gear 3 and facing towards thehousing 3 or the planet carrier 7 during installation has first thrust surfaces 39. The thrust surfaces 39 are formed on the front side of theaxial bulges 42. Thesebulges 42 form trough-like lubrication channels 43 on the rear side of the thrust surfaces 39 and limit an oil passage with theplanet gear 3, which extends through thelubrication channel 43 on the inside from the through-hole 32 radially 30) outwards to theedge 44. - The
second side 46 of thethrust washer 6, which faces theplanet gear 3 and is concealed in the illustration, is provided with second thrust surfaces 38, which are concealed in the illustration and which are formed on the front side of thebulges 41. The front side lies in the direction in which thebulge 41 is axially curved and closes it off axially. In the view shown, thebulges 41form lubrication channels 43 open to the top and, in the installed state (seeFIG. 1 ), together with the planet carrier 7, limit the oil passage, which extends radially outwards on the inside from the through-hole 32 to theedge 44 of thethrust washer 6. In this regard, some of thelubrication channels 43 end radially on the anti-rotation means 8 as seen in the radial direction, which in both cases continues in the radial direction from the radial end of the 41 or 42 in the radial direction projecting beyond thebulge washer body 28. -
FIG. 3 —A view is shown from the axial direction of thethrust washer 6 of a planet bearing 4 in an imaginary and not shown radial plane, wherein the radial plane extends axially between thebase body 33 of thesupport cheek 12 cut out of this view and thethrust washer 6. Thethrust washer 6 is guided on theplanet pin 5 viaedge sections 34 of the through-hole 32 or thewasher body 28. Theedge sections 34 delimit theindentations 30 on the edge in the circumferential direction around theplanetary axis 24. Theindentations 30 connect radially on the inside tolubrication grooves 35 in thethrust washer 6. Therespective planet pin 5 is a planet bolt and is mounted in thesupport cheek 14 visible in the background of the illustration and in the foreground (not shown) in thesupport plate 12. The respectiveplanetary axis 24 extends axially and, in the representation according toFIG. 3 , vertically into the image plane. Aplanet gear 3 follows therespective thrust washer 6 in the viewing direction. Anti-rotation means 8 of athrust washer 6, which is concealed by theplanet gear 3 and arranged axially between theplanet gear 3 and thesupport cheek 14, are visible in the background of the illustration. - The two
thrust washers 6 are provided with the anti-rotation means 8, which protrude radially as tongues from the sheet metal of thethrust washer 6. In this context, the tongues form an angle of 120° between them in a circumferential direction, which can alternatively also be greater or less than 120°. - A
gap 11 is formed between two opposing planet gears 3. One of the connectingpieces 13, which forms one or more of thestops 10, extends between the 12 and 14 in everysupport cheeks gap 11. In this case, thestop 10 is formed on a flank of the connectingpiece 13 facing theplanet gear 3. It is also conceivable that two of the connecting pieces extend in a gap. A pivoting clearance is formed between the anti-rotation means 8 and 30) the connectingpieces 13, by which thethrust washer 6 can pivot on the planet bolt about theplanetary axis 24 up to therespective stop 10 so that one of the anti-rotation means 8 of the respective thrust washer can abut against thestop 10 opposite to it or none of the anti-rotation means 10 can come into contact.Lubrication channels 43 formed in thethrust washer 6 are visible here. -
FIG. 4 —Aplanetary gearbox 21 with ahousing 2, planet gears 3 andplanet bearings 4 a is shown. Thehousing 2 is a planet carrier 7, which is formed from a case-like support cheek 12 and asupport cheek 14 with aflange 25. A plate-like base body 33 of thesupport cheek 12 is provided with axially aligned connectingpieces 13. Thesupport cheek 12 is connected to thesupport cheek 14 via the connectingpieces 13. Theflange 25 has through-holes 26 for fastening theplanetary gearbox 21. - Pocket-
like windows 27 are formed between the connectingpieces 13. Thetoothing 29 of aplanet gear 3 protrudes from each of thewindows 27. The planet gears 3 are arranged axially between thesupport cheek 12 and thesupport cheek 14 and are distributed at equal distances from one another in the case of thesupport cheek 12. The planet gears 3 are mounted withplanet pins 5 on one side in thesupport cheek 12 and on the other side in thesupport cheek 14. The planet gears 3 are rotatably mounted on thehousing 2 by means of theplanet bearings 4 a. The respective planet bearing 4 a is formed from the axially aligned planet pin/planet bolt 5 and athrust washer 6 a. Thethrust washer 6 a sits axially between theplanet gear 3 and thehousing 2 on theplanet pin 5, is provided with two anti-rotation means 8 a, and is held by these anti-rotation means 8 a against rotation relative to thehousing 2 in a form-fitting manner against astop 10 a. - The
stop 10 a is formed circumferentially between two adjacent connectingpieces 13 and projects radially beyond a contour of thebase body 33 of thesupport cheek 12, adjoining theplanet pin 5 radially on the outside, when viewed in the radial direction from the center of theplanetary gearbox 21. More precisely, thestops 10 a for, in each case, one of thethrust washers 6 a are circumferentially formed on the flanks of the planet carrier 7 facing away from one another between two adjacent connectingpieces 13 and adjoining therespective planet pin 5. The flanks are body edges or surfaces, directed in the circumferential direction, of a radially projecting support section of thesupport cheek 12, at which the planet pins 5 are partly accommodated in thesupport cheek 12. -
FIG. 5 —The illustration shows sections of thehousing 2 formed as a planet carrier 7, thesupport cheek 14 and thesupport cheek 12. Therespective stop 10 a projecting radially from thebase body 33 has stop surfaces 19 and 20. A partial surface of the 19 or 20 is opposite the flank of a connectingrespective stop surface piece 13. A first anti-rotation means 8 a formed on therespective thrust washer 6 a in the form of a tongue curved in the manner of a wing at the end engages behind thestop 10 a on afirst stop side 19. A further tongue of a further anti-rotation means 8 a also curved in the manner of a wing at the end engages behind asecond stop side 20 of thestop 10 a in the opposite circumferential direction, which stop side faces away from thefirst stop side 19 in the circumferential direction. Thewings 22 of the anti-rotation means 8 a are angled slightly in an axial direction for this purpose. -
FIG. 7 —The design of theplanetary gearbox 50 is comparable to that of theplanetary gearbox 1 shown inFIG. 1 , with the exception of differently designedthrust washers 48, i.e., thethrust washers 6 of theplanetary gearbox 1 shown inFIG. 1 can be exchanged for thethrust washers 48 and vice versa without further structural changes. - The thrust washers 48 are provided with lubrication channels 51 formed by lubrication grooves 52, each of which ends at an anti-rotation means 49 and, where the anti-rotation means 49 are no longer axially opposite the
housing 2, continues in a lubrication groove 52 to the end of the anti-rotation means 49. -
FIGS. 8, 9 and 10 —The thrust washer has first bulges 53 andsecond bulges 54 circumferentially adjacent to thefirst bulges 53. The bulges are axial recesses created by embossing from a disc-like washer body 55 lying flat in a radial plane. In the exemplary embodiment discussed here, thefirst bulges 53 are curved vertically into the image plane in the representation according toFIG. 8 and are curved out axially to the left from the radial plane E1 according to the representation ofFIG. 9 . In the representation shown inFIG. 8 , thesecond bulges 54 rise vertically into the image plane towards the viewer and are correspondingly curved out axially to the right from the radial plane E2 according to the representation ofFIG. 10 . First thrust surfaces 38 are formed on the front side of thefirst bulges 53, each of which is concealed behind therear side 53 a of thebulge 53 in the representation according toFIG. 8 . The thrust surfaces 39 are formed on the front side of thesecond bulges 54. As a result, the thrust surfaces 39 are, in each case, separated from one another by abulge 53 and the thrust surfaces 38 are separated by abulge 54. Afirst bulge 53 and asecond bulge 54 are, in each case, connected to one another by an elbowedsection 45. -
FIG. 8 —Thethrust washer 48 has two anti-rotation means 49 extending radially from awasher body 55 and formed circumferentially around the center axis or axis ofsymmetry 24 of a planet gear adjacent to one another on thewasher body 55, which are formed integrally/in one piece with thewasher body 55. - The contour of the anti-rotation means 49 projects radially beyond an outer circumferential line U of the
washer body 55 of thethrust washer 48. In this case, thewasher body 55 is annularly delimited on the inside by the contours of the through-hole with theindentations 30 and on the outside by the outer circumferential line U and has an outer diameter DU of the outer circumferential line U. In addition, thewasher body 55 is designed to be symmetrical with respect to the axes of symmetry S1 and S2. The axis of symmetry S1 is aligned horizontally and the axis of symmetry S2 is aligned vertically. The axes of symmetry S1 and S2 lie in a radial plane which is pierced perpendicularly by theplanetary axis 24. The axes of symmetry S1 and S2 extend perpendicular to one another and intersect at a common point on theplanetary axis 24. - The contour of the anti-rotation means 49 is defined, in each case, by two flank lines F1 and F2. Each contour of one of the anti-rotation means 49 is therefore outlined in the image plane by a flank line F1 and a flank line F2 as well as an arc. The arc connects the flank lines F1 and F2 of an anti-rotation means 49. The anti-rotation means 49 are designed to be symmetrical to one another and are mirrored on the axis of symmetry S2. In this regard, the extensions of the flank lines F1 of the two anti-rotation means 49 intersect at a common intersection point C1, which lies on the extension of the axis of symmetry S2 and which lies, at a radial distance from the outer contour of the
thrust washer 48, outside of the outer contour. In this regard, the flank lines F1 and F1 of the adjacent anti-rotation means 49 form an obtuse angle W1 between them and the flank lines F1 and F2 form an acute angle W2 between them and the axis of symmetry S2 on one of the anti-rotation means 49 in each case. The two flank lines F1 of both anti-rotation means 49 optionally merge at a straight line describing the outer contour of the thrust washer at this point and extending radially below the intersection point C1 or alternatively at an arcuate line (not shown) of the outer contour of thethrust washer 48. - The respective extension of the flank line F1 of the one anti-rotation means 49 intersects the extension of its flank line F2 at an intersection point C2, which lies on the axis of symmetry S1 and radially outside of the outer contour of the
thrust washer 48. The contour lines F1 and F2 of the respective anti-rotation means 49 form an acute angle W2 between them. - The
thrust washer 48 is geometrically divided intoquarter sections 48 a-48 d. Thequarter sections 48 a-48 d adjoin one another at the axes of symmetry S1 and S2 and are designed to be symmetrical to one another on thewasher body 55 described by the circumferential line U. Outside of the circumferential line U, the outer contours of the quarter 30) 48 a and 48 b lying above the axis of symmetry S1 are each delimited radially outwards by a complete flank line F1 and a part of a flank line F2. Below the axis of symmetry S1, the outer contours of thesections 48 c and 48 d are each delimited by a part of a flank line F2 and a part of an arc line. The arc line lies on the circumferential line U. The respective flank line F2 merges into the arc line in thequarter sections 48 c and 48 d, so that the contours of the anti-rotation means also extend, in each case, into therespective quarter section 48 c or 48 d lying below the axis of symmetry S1. The radius of the arc line starting from thequarter section planetary axis 24 corresponds to half the diameter DU of the outer circumferential line. - In each of the
quarter sections 48 a-48 d, one of thebulges 54 is fully formed once. Each of thequarter sections 48 a-48 d also has, twice in each case, a part of one of thebulges 53. In this regard, thebulges 54 of the 48 a and 48 b continue in the anti-rotation means 49 up to the outer contour of thequarter sections thrust washer 48 and thus the anti-rotation means 49 at that point. In addition, abulge 53, which extends along the axis of symmetry S1 and is formed partially in a 48 a and 48 d or 48 b and 48 d, continues radially outwards as far as the outer contour of the respective anti-rotation means 49 and thus the outer contour of thequarter section thrust washer 48. This means that in the planetary gearbox shown inFIG. 7 , at least one lubrication channel (43) delimited on at least one side by the thrust washer (48) extends radially outwards to partial sections of the contour lines F1, F2 of the outer contours of the anti-rotation means 49 delimiting the anti-rotation means 49 radially on the outside—i.e., that thelubrication channel 43 or the 53, 54 continue radially to the end/to the tip of the anti-rotation means 49 via the contact with the planet gear and/or the planet carrier.bulges -
FIGS. 9 and 10 —The sheet metal of thethrust washer 48 has a sheet thickness D. The total thickness A of thethrust washer 48 is composed of the sheet thickness D and the axial offset T. The axial offset T is a measure of the depth of the 53 and 54 and is less than the sheet thickness D in this case.bulges -
-
- 1 Planetary gearbox
- 2 Housing
- 3 Planet gear
- 4 Planet bearing
- 4 a Planet bearing
- 5 Planet pin
- 6 Thrust washer
- 6 a Thrust washer
- 7 Planet carrier
- 8 Anti-rotation means
- 8 a Anti-rotation means
- 9 Central axis
- 10 Stop
- 10 a Stop
- 11 Gap between the planet gears
- 12 Support cheek of the planet carrier
- 13 Connecting piece of the planet carrier
- 14 Support cheek of the planet carrier
- 15 Not assigned
- 16 First side of the thrust washer
- 17 Second side of the thrust washer
- 18 Contour of the planet gear or toothing of the planet gear
- 19 First stop side
- 20 Second stop side
- 21 Planetary gearbox
- 22 Wing of the anti-rotation means
- 23 Stop
- 24 Planetary axis
- 25 Flange of the support cheek
- 26 Through-hole of the flange
- 27 Window
- 28 Washer body of the thrust washer
- 29 Toothing of the planet gear
- 30 Indentations on the thrust washer
- 31 Recesses in the thrust washer
- 32 Through-hole in the thrust washer
- 33 Base body of the support cheek
- 34 Edge section
- 35 Lubrication groove
- 36 Not assigned
- 37 Not assigned48
- 38 Second thrust surface of the thrust washer
- 39 First thrust surface of the thrust washer
- 40 First side of the thrust washer
- 41 First bulge of the thrust washer
- 42 Second bulge of the thrust washer
- 43 Lubrication channel on the thrust washer
- 44 Edge of the thrust washer
- 45 Elbowed section of the thrust washer
- 46 Second side of the thrust washer
- 47 Not assigned
- 48 Thrust washer
- 48 Quarter section of the thrust washer
- 48 b Quarter section of the thrust washer
- 48 c Quarter section of the thrust washer
- 48 d Quarter section of the thrust washer
- 49 Anti-rotation means
- 50 Planetary gearbox?
- 51 Lubrication channel
- 52 Lubrication groove
- 53 First bulge on the thrust washer
- 53 a Rear side of the bulge
- 54 Second bulge on the thrust washer
- 55 Washer body of the thrust washer
- A Axial offset
- C1 Intersection point of the flank lines
- C2 Intersection point of the flank lines
- D Sheet thickness
- DU Diameter of the outer circumferential line
- F1 Flank line
- F2 Flank line
- G Straight line
- S1 Axis of symmetry
- S2 Axis of symmetry
- T Depth of the bulge
- U Outer circumferential line of the washer body
- W1 Angle between the flank lines
- W2 Angle between the flank lines
Claims (18)
1. A planetary gearbox having a housing, with planet gears and with planet bearings, wherein the planet gears are mounted on the housing by means of the planet bearings so as to be rotatable about an axially aligned planetary axis and wherein at least one of the planet bearings is formed from at least one axially aligned planet pin and a thrust washer, wherein the thrust washer is seated axially between the planet gear and the housing on the planet pin and is secured so as to prevent rotation about the planetary axis with the aid of two anti-rotation means formed on the thrust washer, and wherein each of the anti-rotation means faces a stop of the housing, wherein the thrust washer has first thrust surfaces on a first side facing the housing and second thrust surfaces offset circumferentially relative to the first thrust surfaces on a second side facing a planet gear, wherein trough-like lubrication channels are formed on the thrust washer axially on rear sides of the first and second thrust surfaces, and wherein the lubrication channels extend radially outwards from the direction of the planet pin as far as an edge of the thrust washer which delimits the thrust washer radially on an outside.
2. The planetary gearbox according to claim 1 , wherein each of the lubrication channels extends between two of the first thrust surfaces of the thrust washer which are circumferentially adjacent to one another.
3. The planetary gearbox according to claim 1 , wherein the each of the lubrication channels ends at at least one of the anti-rotation means of a thrust washer.
4. The planetary gearbox according to claim 1 , in which at least one housing section of the housing is formed as a planet carrier with at least two support cheeks of the planet carrier connected axially via connecting pieces, wherein the stop is a connecting piece projecting axially from one support cheek of the planet carrier in the direction of a further support cheek.
5. The planetary gearbox according to claim 4 , wherein each of the connecting pieces has at least one stop for one anti-rotation means formed on one and the same thrust washer of two anti-rotation means formed on the thrust washer.
6. The planetary gearbox according to claim 1 , in which at least one housing section of the housing is formed as a planet carrier with at least two support cheeks, and the support cheeks are connected axially by means of connecting pieces, wherein two flanks of the planet carrier facing away from one another are the stops for the anti-rotation means of a thrust washer, and wherein the stops are formed circumferentially between two adjacent connecting pieces and thereby circumferentially adjoining the planet pin.
7. The planetary gearbox according to claim 1 , wherein the thrust washer has two anti-rotation means which extend radially from a washer body and are formed circumferentially about a planetary axis of a planet gear adjacent to one another on the washer body and are made of a material of the thrust washer, and wherein a first anti-rotation means rests against a first stop and a second anti-rotation means formed on the same thrust washer rests against a second stop opposite the first stop or facing away from this first stop.
8. The planetary gearbox according to claim 1 , wherein at least one of the anti-rotation means projects radially away from the planet pin beyond a contour of at least one planet gear, which contour delimits the at least one planet gear on an outside.
9. The planetary gearbox according to claim 8 , wherein the lubrication channels extend radially outwards as far as at least one contour line, which delimits the anti-rotation means radially on an outside.
10. A thrust washer for a planetary gearbox, according to claim 1 , wherein the thrust washer has two anti-rotation means which extend radially from a washer body and are formed circumferentially about an axis of symmetry of the washer body adjacent to one another on the washer body and are made of a material of the thrust washer, wherein the anti-rotation means are projections projecting radially beyond an outer circumference of a washer body of the thrust washer, wherein the thrust washer has first bulges and second bulges circumferentially adjacent to the first bulges, wherein thrust surfaces for sliding contact with a planet carrier or a planet gear are formed on each of the first and second bulges.
11. A planetary gearbox comprising:
a housing comprising a pair of stops;
a planet bearing mounted in the housing and formed from an axially aligned planet pin and a thrust washer; and
a planet gear rotatable about a planetary axis on the planet bearing, wherein the thrust washer comprises:
an outer circumferential surface;
two integrally-formed projections, each facing a one of the pair of stops to prevent rotation of the thrust washer about the planetary axis and extending radially beyond the outer circumferential surface;
first thrust surfaces disposed on a first side of the thrust washer facing the housing;
first lubrication channels formed axially opposite the first thrust surfaces and extending radially outwards;
second thrust surfaces circumferentially offset from the first thrust surfaces and disposed on a second side of the thrust washer facing the planet gear; and
second lubrication channels formed axially opposite the second thrust surfaces and extending radially outwards.
12. The planetary gearbox of claim 11 , wherein the second lubrication channels extend between circumferentially adjacent first thrust surfaces.
13. The planetary gearbox of claim 11 , wherein the projections project radially away from the planet pin beyond an outer contour of the planet gear.
14. The planetary gearbox of claim 11 , wherein:
the housing comprises a housing section formed as a planet carrier;
the planet carrier comprises two axially offset support cheeks connected by connecting pieces; and
the connecting pieces form the pair of stops.
15. The planetary gearbox of claim 11 , wherein:
the two integrally-formed projections are tongue-like projections; and
a one of the second lubrication channels ends at a one of the tongue-like projections.
16. The planetary gearbox of claim 11 , wherein:
the two integrally-formed projections are bulges; and
a one of the second lubrication channels extends to a flank line delimiting a radial outside of a one of the bulges.
17. A planetary gearbox comprising:
a housing comprising a pair of stops;
a planet bearing mounted in the housing and formed from an axially aligned planet pin and a thrust washer; and
a planet gear rotatable about a planetary axis on the planet bearing, wherein the thrust washer comprises:
two integrally-formed tongue-like projections curved in the manner of a wing, each wing engaged behind a one of the pair of stops to prevent rotation of the thrust washer about the planetary axis;
a radially outer surface;
first thrust surfaces disposed on a first side of the thrust washer facing the housing and first lubrication channels formed axially opposite the first thrust surfaces and extending radially outwards to the radially outer surface; and
second thrust surfaces circumferentially offset from the first thrust surfaces and disposed on a second side of the thrust washer facing the planet gear and second lubrication channels formed axially opposite the second thrust surfaces and extending radially outwards to the radially outer surface.
18. The planetary gearbox of claim 16 , wherein:
the housing comprises a housing section formed as a planet carrier;
the planet carrier comprises:
two axially offset support cheeks connected by connecting pieces; and
two flanks facing away from one another and formed circumferentially between two circumferentially adjacent connecting pieces; and
the two flanks form the pair of stops.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102021131137 | 2021-11-26 | ||
| DE102021131137.3 | 2021-11-26 | ||
| PCT/DE2022/100868 WO2023093939A1 (en) | 2021-11-26 | 2022-11-21 | Planetary gearbox with a thrust washer having anti-rotation means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20250003483A1 true US20250003483A1 (en) | 2025-01-02 |
Family
ID=84365524
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US18/710,328 Pending US20250003483A1 (en) | 2021-11-26 | 2022-11-21 | Planetary gearbox with a thrust washer having anti-rotation means |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20250003483A1 (en) |
| EP (1) | EP4437242A1 (en) |
| CN (1) | CN118318108A (en) |
| DE (1) | DE112022005648A5 (en) |
| WO (1) | WO2023093939A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20240426339A1 (en) * | 2023-06-23 | 2024-12-26 | E. Winkemann Gmbh | Thrust Washer for Distributing a Fluid with Lubricant Pockets |
| US20250189028A1 (en) * | 2022-08-24 | 2025-06-12 | Eaton Intelligent Power Limited | Compact direct-acting e-locker and methods therefor |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102022110183A1 (en) | 2022-04-27 | 2023-11-02 | Schaeffler Technologies AG & Co. KG | Planetary gear with a rotation-proof thrust washer on the planetary bearing |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5695424A (en) * | 1994-10-28 | 1997-12-09 | Jatco Corporation | Planetary carrier having a porous washer |
| DE102004014578A1 (en) * | 2004-03-25 | 2005-12-15 | Zf Friedrichshafen Ag | planetary gear |
| US20140194244A1 (en) * | 2013-01-10 | 2014-07-10 | Zf Friedrichshafen Ag | Axial bearing of pinion gears of a planetary gear set |
| KR20170058478A (en) * | 2015-11-18 | 2017-05-29 | 현대 파워텍 주식회사 | Planetary gear apparatus |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2527161Y2 (en) | 1989-03-28 | 1997-02-26 | ジャトコ 株式会社 | Carrier assembly of planetary gear set |
| JP2001082456A (en) * | 1999-09-13 | 2001-03-27 | Shin Kobe Electric Mach Co Ltd | Thrust washer |
| US7252615B2 (en) * | 2004-03-22 | 2007-08-07 | General Motors Corporation | Lubrication system and method for hybrid electro-mechanical planetary transmission components |
| DE102013104129B3 (en) * | 2013-04-24 | 2014-07-03 | E. Winkemann Gmbh | Thrust washer with lubricant pockets |
-
2022
- 2022-11-21 CN CN202280075947.1A patent/CN118318108A/en active Pending
- 2022-11-21 DE DE112022005648.7T patent/DE112022005648A5/en not_active Withdrawn
- 2022-11-21 US US18/710,328 patent/US20250003483A1/en active Pending
- 2022-11-21 EP EP22813890.5A patent/EP4437242A1/en active Pending
- 2022-11-21 WO PCT/DE2022/100868 patent/WO2023093939A1/en not_active Ceased
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5695424A (en) * | 1994-10-28 | 1997-12-09 | Jatco Corporation | Planetary carrier having a porous washer |
| DE102004014578A1 (en) * | 2004-03-25 | 2005-12-15 | Zf Friedrichshafen Ag | planetary gear |
| US20140194244A1 (en) * | 2013-01-10 | 2014-07-10 | Zf Friedrichshafen Ag | Axial bearing of pinion gears of a planetary gear set |
| US8992369B2 (en) * | 2013-01-10 | 2015-03-31 | Zf Friedrichshafen Ag | Axial bearing of pinion gears of a planetary gear set |
| KR20170058478A (en) * | 2015-11-18 | 2017-05-29 | 현대 파워텍 주식회사 | Planetary gear apparatus |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20250189028A1 (en) * | 2022-08-24 | 2025-06-12 | Eaton Intelligent Power Limited | Compact direct-acting e-locker and methods therefor |
| US20240426339A1 (en) * | 2023-06-23 | 2024-12-26 | E. Winkemann Gmbh | Thrust Washer for Distributing a Fluid with Lubricant Pockets |
Also Published As
| Publication number | Publication date |
|---|---|
| DE112022005648A5 (en) | 2024-09-12 |
| WO2023093939A1 (en) | 2023-06-01 |
| EP4437242A1 (en) | 2024-10-02 |
| CN118318108A (en) | 2024-07-09 |
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